CA2874920A1 - Procede de realisation d'un caisson central de voilure - Google Patents
Procede de realisation d'un caisson central de voilure Download PDFInfo
- Publication number
- CA2874920A1 CA2874920A1 CA2874920A CA2874920A CA2874920A1 CA 2874920 A1 CA2874920 A1 CA 2874920A1 CA 2874920 A CA2874920 A CA 2874920A CA 2874920 A CA2874920 A CA 2874920A CA 2874920 A1 CA2874920 A1 CA 2874920A1
- Authority
- CA
- Canada
- Prior art keywords
- spar
- central wing
- wing box
- panel
- producing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 238000004519 manufacturing process Methods 0.000 title description 3
- 239000003351 stiffener Substances 0.000 claims description 23
- 238000000034 method Methods 0.000 claims description 13
- 229910052751 metal Inorganic materials 0.000 claims description 10
- 239000002184 metal Substances 0.000 claims description 10
- 238000003754 machining Methods 0.000 claims description 6
- 238000003466 welding Methods 0.000 claims description 6
- 229910000838 Al alloy Inorganic materials 0.000 description 3
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- 229910001148 Al-Li alloy Inorganic materials 0.000 description 1
- JFBZPFYRPYOZCQ-UHFFFAOYSA-N [Li].[Al] Chemical compound [Li].[Al] JFBZPFYRPYOZCQ-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 235000000396 iron Nutrition 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/182—Stringers, longerons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/12—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding
- B23K20/129—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by friction; Friction welding specially adapted for particular articles or workpieces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49616—Structural member making
- Y10T29/49622—Vehicular structural member making
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Body Structure For Vehicles (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Bending Of Plates, Rods, And Pipes (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1363133A FR3015426B1 (fr) | 2013-12-20 | 2013-12-20 | Procede de realisation d'un caisson central de voilure |
FR1363133 | 2013-12-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA2874920A1 true CA2874920A1 (fr) | 2015-06-20 |
Family
ID=50483020
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2874920A Abandoned CA2874920A1 (fr) | 2013-12-20 | 2014-12-10 | Procede de realisation d'un caisson central de voilure |
Country Status (5)
Country | Link |
---|---|
US (1) | US20150175252A1 (ja) |
JP (1) | JP2015227154A (ja) |
CN (1) | CN104724278A (ja) |
CA (1) | CA2874920A1 (ja) |
FR (1) | FR3015426B1 (ja) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB201508375D0 (en) | 2015-05-15 | 2015-07-01 | Airbus Operations Ltd | Method of forming composite structures |
US10479474B2 (en) | 2016-07-14 | 2019-11-19 | The Boeing Company | Friction stir welded wingtip torque box |
US10875625B2 (en) * | 2017-08-23 | 2020-12-29 | The Boeing Company | Co-cured spar and stringer center wing box |
CN111328792B (zh) * | 2020-04-15 | 2023-06-30 | 徐州新南湖科技有限公司 | 一种植保无人机防风撒药器 |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4749155A (en) * | 1985-09-30 | 1988-06-07 | The Boeing Company | Method of making wing box cover panel |
US6036802A (en) * | 1996-09-13 | 2000-03-14 | The Boeing Company | Thermoplastic panel bending |
CA2298005C (en) * | 1998-05-25 | 2004-02-03 | Prospective Concepts Ag | Adaptive pneumatic wings for flying devices with fixed wings |
JP2000006893A (ja) * | 1998-06-23 | 2000-01-11 | Fuji Heavy Ind Ltd | 複合材翼構造 |
US6655633B1 (en) * | 2000-01-21 | 2003-12-02 | W. Cullen Chapman, Jr. | Tubular members integrated to form a structure |
US8515677B1 (en) * | 2002-08-15 | 2013-08-20 | Smart Drilling And Completion, Inc. | Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials |
JP4065156B2 (ja) * | 2002-07-17 | 2008-03-19 | 本田技研工業株式会社 | 航空機用翼体の製造方法 |
US8156711B2 (en) * | 2003-02-24 | 2012-04-17 | Bell Helicopter Textron Inc. | Contact stiffeners for structural skins |
CA2529108C (en) * | 2004-12-07 | 2012-10-30 | Airbus Deutschland Gmbh | Airplane wing, method for manufacturing an airplane wing and use of a welding process for welding a wing spar |
FR2901240B1 (fr) * | 2006-05-17 | 2009-01-09 | Airbus France Sas | Poutre interne composite pour renforcer la structure d'un aeronef |
BRPI0721604B1 (pt) * | 2007-04-30 | 2018-06-26 | Airbus Operations, S.L. | Método para a fabricação de uma estrutura de caixa de torção de multilongarinas integradas de material compósito para aeronave |
WO2008145527A1 (en) * | 2007-05-31 | 2008-12-04 | Airbus Operations Gmbh | Method for producing a composite skin in the field of aeronautics and astronautics |
FR2948099B1 (fr) * | 2009-07-16 | 2012-05-11 | Airbus Operations Sas | Procede de fabrication d'un aeronef a voilure fixe |
GB201008186D0 (en) * | 2010-05-17 | 2010-06-30 | Airbus Operations Ltd | A structural assembly for an aircraft |
FR2962409B1 (fr) * | 2010-07-09 | 2012-09-21 | Airbus Operations Sas | Procede de realisation d'un caisson central de voilure |
GB201103125D0 (en) * | 2011-02-23 | 2011-04-06 | Airbus Uk Ltd | Composite structure |
CN102514708B (zh) * | 2011-10-26 | 2015-03-18 | 中国商用飞机有限责任公司 | 一种整体式复合材料中央翼盒 |
US9434466B2 (en) * | 2011-11-30 | 2016-09-06 | Airbus Sas | Component having a box structure for an airplane airfoil |
GB201204231D0 (en) * | 2012-03-09 | 2012-04-25 | Airbus Uk Ltd | Space frame structure |
-
2013
- 2013-12-20 FR FR1363133A patent/FR3015426B1/fr active Active
-
2014
- 2014-12-09 JP JP2014249283A patent/JP2015227154A/ja active Pending
- 2014-12-10 CA CA2874920A patent/CA2874920A1/fr not_active Abandoned
- 2014-12-11 US US14/566,822 patent/US20150175252A1/en not_active Abandoned
- 2014-12-18 CN CN201410799156.0A patent/CN104724278A/zh active Pending
Also Published As
Publication number | Publication date |
---|---|
CN104724278A (zh) | 2015-06-24 |
JP2015227154A (ja) | 2015-12-17 |
FR3015426A1 (fr) | 2015-06-26 |
US20150175252A1 (en) | 2015-06-25 |
FR3015426B1 (fr) | 2017-10-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FZDE | Discontinued |
Effective date: 20210302 |